THRUST IS: Rocky Morey: Drummer - 23 years old. Originally from Troy, NY. Computer Specialist and Programmer for Albany Medical Center. He has Computer Science degrees from Hudson Valley Community College, and NRI in Washington DC. He is currently studying CS at Rensselaer Polytechnic Institute. Rocky has played the drums since he was 3 years old, receiving professional tutelage for 14 years in a wide range of styles...
|IUMA: Thrust SuperSonic|
Thrust SuperSonic Where did they come from? Well, after finding some great musicians to work with, Brandon formed Thrust SuperSonic in 1997. With a new and more powerful sound in Thrust SuperSonic, the they have pushed the envelope. The band consists of three very talented musicians - Barry Kerch on drums, Chris Marcelli on bass, and Brandon on guitar and lead vocals. With a hard edge original music, this trio has put together one of the best bands around...
Keywords: Thrust SuperSonic
|C64-Gamevideoarchive 273 - Thrust - The C64-Gamevideoarchive|
Video from the C64 game "Thrust" >>Download Video (75 MB)
Keywords: c64; thrust
|Thrust Vectoring, High Alpha Research - NASA|
The center used an F-18 as the High Angle-of-Attack Research Vehicle in a program from 1987 to 1996. Fresh from its reconstruction (it was assembled from many parts and affectionately dubbed "Silk Purse"), the aircraft was extensively instrumented both to record data at high angles of attack and as a means of developing flight research techniques in high-alpha flight. Researchers also conducted visual studies of the airflow over various parts of the aircraft at high alpha using tracer smoke, tuf...
Keywords: Thrust Vectoring, High Alpha Research
|Transient and steady performance of an ion rocket thrust augmentor Summary report - NON|
Transient and steady performance of ion rocket thrust augmentor
Keywords: AUGMENTATION; ION PROPULSION; IONIZERS; ROCKET THRUST; THRUST AUGMENTATION; IONIC PROPULSION; THRUST AUGMENTATION
|Analytical calculation of a single jet in cross-flow and comparison with experiment - Claus, R. W|
A series of progressively finer grid systems to calculate the single jet in cross-flow experimentally measured were employed. The experimental measurements provide a collection of velocities, turbulence intensities, and jet concentration profiles with measurements of the inlet field. The use of a series of progressively finer grid systems allows a differentiation between numerical errors and the hydrodynamic modeling assumptions embodied in the 3D combustor code.
Keywords: EXHAUST NOZZLES; THRUST REVERSAL; THRUST VECTOR CONTROL; TURBOJET ENGINES; COOLING; LEAKAGE; NOZZLE THRUST COEFFICIENTS; STATIC PRESSURE; THREE DIMENSIONAL FLOW
|Transonic static aerodynamic characteristics of a blunt cone-cylinder body with flared afterbody or blunt cruciform fins - Knechtel, E. D.|
No Abstract Available
Keywords: BALLISTIC MISSILES; MISS DISTANCE; ROTATION; THRUST TERMINATION; THRUST VECTOR CONTROL; MISSILE BODIES; ROTATING BODIES; THRUST REVERSAL; TRAJECTORY ANALYSIS
|A study of low-thrust guidance - Ash, G. R|
Mathematical statement and computer simulation of low thrust guidance problem - minimum time solutions
Keywords: COMPUTERIZED SIMULATION; TIME FUNCTION; FORMULATIONS; GUIDANCE (MOTION); LOW THRUST; LOW THRUST PROPULSION; TIME FUNCTIONS; COMPUTER SIMULATION; GUIDANCE; LOW THRUST PROPULSION
|THRUST CHAMBER COOLING TECHNIQUES FOR SPACECRAFT ENGINES, VOLUME II - Batha, D. R.|
Cooling liquid propellant rocket engine thrust chambers - data & bibliography
Keywords: ABLATION; COOLING; LIQUID PROPELLANT ROCKET ENGINES; THRUST; THRUST CHAMBERS; BIBLIOGRAPHY; COOLING; LIQUID PROPELLANT ROCKET ENGINE; THRUST CHAMBER
|COMPUTATION OF PLUG NOZZLE CONTOURS BY THE RAO OPTIMUM THRUST METHOD - Lee, C. C|
Fortran computer program to design plug nozzle by using rao maximum thrust theory
Keywords: COMPUTER PROGRAMS; OPTIMUM THRUST PROGRAMMING; CONTOURS; EULER-LAGRANGE EQUATION; FORTRAN; PLUG NOZZLES; THRUST; THRUST PROGRAMMING; FORTRAN; NOZZLE
|The GameSparked Podcast Feb-21-2012|
Keywords: gamesparked; video games; twisted metal; pelvic thrust
|Reliability Assessment of a Robust Design Under Uncertainty for a 3-D Flexible Wing - Gumbert, Clyde R.|
The paper presents reliability assessment results for the robust designs under uncertainty of a 3-D flexible wing previously reported by the authors. Reliability assessments (additional optimization problems) of the active constraints at the various probabilistic robust design points are obtained and compared with the constraint values or target constraint probabilities specified in the robust design...
Keywords: TURBOJET ENGINES; DUCTS; SHROUDS; PRESSURE MEASUREMENT; THRUST
|TVC jet vane thermal modeling using parametric system identification - Nunn, R. H. (Robert H.).|
Title from cover
Keywords: JET VANES; THRUST VECTOR CONTROL SYSTEMS
|Effect of initial mixture temperature on flame speeds and blow-off limits of propane - air flames - Dugger, Gordon|
No Abstract Available
Keywords: HELICOPTERS, COAXIAL; PROPELLERS, HELICOPTER - THRUST, STATIC
|Experiments with rotating, 10-inch diameter externally pressurized air thrust bearings - Anderson, W. J.|
No Abstract Available
Keywords: GAS BEARINGS; PARABOLIC REFLECTORS; ROTATION; THRUST BEARINGS
|NASA Connect - SOF - Forces of Flight - NASA LaRC Office of Education|
NASA Connect segment explainging the fundamentals of flight and the science behind it.
Keywords: NASA Connect; Flights; Thrust; Weight; Lift; Drag
|Interplanetary Trajectories and Payload Capabilities of Advanced Propulsion Vehicles - Melbourne, W. G|
No Abstract Available
Keywords: INTERPLANETARY TRAJECTORIES; LOW THRUST; PAYLOADS; PROPULSION
"Thrust" documented the street music scene in Florida from 1989 to 1993 out of Tampa Bay, FL. This monthly free publication brought "...a new breed of rock journalism that is unprecedented in the Tampa Bay area -- hard hitting and deep pounding."
Keywords: Thrust magazine Florida Tampa Bay bi-coastal
|A wave-envelope of sound propagation in nonuniform circular ducts with compressible mean flows - Nayfeh, A. H.|
An acoustic theory is developed to determine the sound transmission and attenuation through an infinite, hard-walled or lined circular duct carrying compressible, sheared, mean flows and having a variable cross section. The theory is applicable to large as well as small axial variations, as long as the mean flow does not separate. The technique is based on solving for the envelopes of the quasi-parallel acoustic modes that exist in the duct instead of solving for the actual wave, thereby reducin...
Keywords: ROCKET ENGINES; ROCKET PROPELLANTS; SCIENTISTS; HISTORIES; MATHEMATICAL LOGIC; ROCKET FLIGHT; ROCKET THRUST; THRUST CHAMBERS
|Spray Cooling Trajectory Angle Impact Upon Heat Flux Using a Straight Finned Enhanced Surface - Silk, Eric A.|
Experiments were conducted to study the effects of spray trajectory angles upon heat flux for flat and enhanced surface spray cooling. The surface enhancement consisted of straight fins machined on the top surface of a copper heater block. Spray cooling curves were obtained with the straight fin surface aligned both parallel (axial) and perpendicular (transverse) to the spray axis. Measurements were also obtained on a flat surface heater block for comparison purposes...
Keywords: ACOUSTIC PROPERTIES; GROUND TESTS; PIPES (TUBES); LIQUID OXYGEN; ACOUSTICS; THRUST CHAMBERS; PRESSURE SENSORS; THRUST
|An Autonomous Control System for an Intra-Vehicular Spacecraft Mobile Monitor Prototype - Dorais, Gregory A.|
This paper presents an overview of an ongoing research and development effort at the NASA Ames Research Center to create an autonomous control system for an internal spacecraft autonomous mobile monitor. It primary functions are to provide crew support and perform intra- vehicular sensing activities by autonomously navigating onboard the International Space Station. We describe the mission roles and high-level functional requirements for an autonomous mobile monitor...
Keywords: PULSE DETONATION ENGINES; EJECTORS; THRUST AUGMENTATION; THRUST MEASUREMENT; TEST STANDS; DETONATION; TURBOFAN ENGINES; PRESSURE SENSORS
|The pharmacological approach to the study of the mechanisms regulating ACTH secretion - Vernikos-Danellis, J|
Catecholamine effects on regulating ACTH secretions
Keywords: AERODYNAMIC CHARACTERISTICS; JET FLAPS; SCALE MODELS; THRUST AUGMENTATION; EJECTORS; JET THRUST; LIFT
|Investigations of space storable propellants first interim summary report, mar. 1963 - jan. 1964 - Luperi, M|
Injector configurations and ablative thrust chamber materials for use with oxygen difluoride- diborane propellant combinations
Keywords: ABLATION; DIBORANE; INJECTOR; THRUST CHAMBER; ABLATIVE MATERIALS; DIBORANE; DIFLUORIDES; INJECTORS; OXYGEN; PROPELLANTS; STORABLE PROPELLANTS; THRUST CHAMBERS
|Aeroelastic stability of plane sandwich-type structures placed in a current of supersonic gas - Librescu, L., et al|
Linear formulation of aeroelastic stability of plane sandwich-type structures placed in current of supersonic gas
Keywords: AIRCRAFT STABILITY; ENGINE DESIGN; THRUST CONTROL; V/STOL AIRCRAFT; AIRCRAFT CONTROL; GLIDING; THRUST MEASUREMENT
|Motion cues in man-vehicle control - Shirley, R. S.|
Human operator using roll angular motion cues in man vehicle control
Keywords: EXPERIMENT DESIGN; FUEL INJECTION; THRUST CHAMBER PRESSURE; PERFORMANCE TESTS; THRUST CHAMBERS
|Effects on longitudinal stability and control characteristics of a B-29 airplane of variations in stick-force and control-rate characteristics obtained through use of a booster in the elevator-control system - Mathews, Charles W|
The longitudinal stability and control characteristics of a B-29 airplane have been measured with a control surface booster incorporated in the elevator-control system. The measurements were obtained with the booster operating to provide various control-force gradients and various maximum rates of control motion. Results are presented which show the effect of these booster parameters on the handling qualities of the test airplane.
Keywords: ENGINES, TURBOJET - THRUST AUGMENTORS; AFTERBURNING; BLEED-OFF; ENGINES - WATER INJECTION; ENGINES, TURBOJET - THRUST
|GENERAL EXPRESSIONS OF THE DEVELOPMENT IN SERIES OF THE COORDINATES OF A CELESTIAL BODY - CIPOLLETTI, D|
A NUMERICAL ANALYSIS IS PRESENTED OF THE DETERMINATION OF THE ORBITAL ELEMENTS OF A CELESTIAL BODY.
Keywords: JET THRUST; THRUST VECTOR CONTROL; WASTE DISPOSAL; MANNED SPACE FLIGHT; RELIABILITY ENGINEERING; SPACE STATIONS
|Propagation of disturbances above the flow during the interaction of a hypersonic flow with a boundary layer - Neyland, V. YA|
Turbulence diffusion above flow during boundary layer and hypersonic flow interaction
Keywords: ENGINE DESIGN; ION ENGINES; RADIATIVE HEAT TRANSFER; SPACECRAFT CONTROL; THRUST AUGMENTATION; HEAT SHIELDING; THRUST CONTROL
|Analyses for turbojet thrust augmentation with fuel-rich afterburning of hydrogen, diborane, and hydrazine - Morris, J. F|
Turbojet thrust augmentation with fuel-rich afterburning of hydrogen, diborane, and hydrazine
Keywords: AFTERBURNING; DIBORANE; HYDRAZINES; HYDROGEN; THRUST AUGMENTATION; TURBOJET ENGINES; AFTERBURNING; DIBORANE; THRUST AUGMENTATION
|Mars Smart Lander Parachute Simulation Model - Queen, Eric M.|
A multi-body flight simulation for the Mars Smart Lander has been developed that includes six degree-of-freedom rigid-body models for both the supersonically-deployed and subsonically-deployed parachutes. This simulation is designed to be incorporated into a larger simulation of the entire entry, descent and landing (EDL) sequence. The complete end-to-end simulation will provide attitude history predictions of all bodies throughout the flight as well as loads on each of the connecting lines...
Keywords: AUTOMATIC CONTROL; AUTONOMY; THRUST VECTOR CONTROL; FAILURE; TORQUE; YAW; THRUST; ROLL; GIMBALS
|NASA SCI Files - Thrust Experiment - NASA LaRC Office of Education|
NASA Sci Files segment involving students in an activity to measure the limits of vertical thrust.
Keywords: Jennifer Parsons; Green Valley Elementary School; Boone; Hypothesis; Thrust; Activity; Vertical Thrust
|A low-pressure-loss short afterburner for sea-level thrust augmentation - Burley, R. R.|
Low-pressure-loss short afterburner design for sea level thrust augmentation of axial flow turbojet engine
Keywords: AFTERBURNING; AXIAL FLOW; LOW PRESSURE; SEA LEVEL; THRUST AUGMENTATION; TURBOJET ENGINES; AFTERBURNER; THRUST AUGMENTATION; TURBOJET ENGINE
|COMPARISON OF INJECTORS WITH A 200-POUND-THRUST AMMONIA-OXYGEN ENGINE - Clark, B. J.|
Injection techniques for 200-pound thrust ammonia- oxygen rocket engine
Keywords: AMMONIA; INJECTION; LOW THRUST PROPULSION; OXYGEN; ROCKET ENGINE; BOURDON TUBES; INJECTION; INJECTORS; LOW THRUST; LOW THRUST PROPULSION; OXYGEN; ROCKET ENGINES; AMMONIA
|Energy accumulator in optimization problems of spaceflight with limited power - Grodzovskiy, G. L.|
Energy accumulator for optimal control of low- thrust space flight
Keywords: ACCUMULATORS; PROPULSIVE FLUID ACCUMULATOR /PROFAC/; ENERGY STORAGE; LOW THRUST; LOW THRUST PROPULSION; OPTIMAL CONTROL; OPTIMIZATION; SPACE FLIGHT; ENERGY STORAGE DEVICE; LOW THRUST PROPULSION
|COMBINED COMPRESSOR COOLANT INJECTION AND AFTERBURNING FOR TURBOJET THRUST AUGMENTATION - Fenn, D. B.|
Combined compressor coolant injection and afterburning for turbojet engine thrust augmentation
Keywords: AFTERBURNING; TURBOJET ENGINES; AFTERBURNING; COMPRESSOR; COOLANT; INJECTION; PROPULSION; THRUST AUGMENTATION; TURBINE; TURBOJET ENGINE; COMPRESSORS; COOLANTS; INJECTION; MACH NUMBER; PROPULSION; THRUST; THRUST AUGMENTATION; TURBINES
|F-15B ACTIVE with Thrust Vectoring Nozzles - NASA/Jim Ross|
The F-15 ACTIVE in flight over the Mojave desert during a High Stability Engine Control (HISTEC) flight. The twin-engine F-15 is equipped with new Pratt & Whitney nozzles that can turn up to 20 degrees in any direction, giving the aircraft thrust control in the pitch (up and down) and yaw (left and right) directions. On March 27, 1996, NASA began flight testing a new thrust-vectoring concept on the F-15 research aircraft to improve performance and aircraft control...
Keywords: Rocket Propulsion; Unique Aircraft; Thrust Vector Research Aircraft
|Design and development of a thermo-ionic electric thrustor Interim report - Ducati, A. C.|
Propellants and thrust performance for thermoionic electric thrustor
Keywords: ION PROPULSION; PROPELLANTS; THERMOELECTRICITY; THRUST; THRUSTORS; IONIC PROPULSION; THERMOELECTRICITY; THRUSTOR
|Guardian (1994)(Acid Software)|
Guardian (1994)(Acid Software)
Keywords: joypad; dronoids; tracking; guardian; destroy; smart; dronoid; alien; options; thrust
|Effect of Shocks on Mixing and Thrust in Over-expanded Nozzles|
The flow in the divergent part of a highly over-expanded nozzle suffers strong instability due to formation of shock waves which causes mixing enhancement in the flow and destabilizes the shear layer adjacent to it. The code FLUENT has been used to simulate the flow of two different viscous fluids (air and hydrogen) through five different ConvergentDivergent (C-D) nozzles of varying area ratio and exit angles...
Keywords: Lambda Shock; Asymmetry; Mixing; Turbulent Kinetic Energy; Thrust
|Air admixture to exhaust jets - United States.: National Advisory Committee for Aeronautics|
Keywords: Aerodynamics; Rocket engines--Exhaust emissions; Rocket engines--Thrust
|Commodore 16 Games Pack I (1984)(Melbourne House)|
Commodore 16 Games Pack I (1984)(Melbourne House)
Keywords: games; ffi; thrust; otjfj; cdc; landa; oco; spacecral; ceo; odou
|NASA SCI Files - Thrust - NASA LaRC Office of Education|
NASA Sci Files segment demonstrating, through the Airbus A320 Flight Simulator, the power and control of thrust.
Keywords: Simulator; AIRBUS A320; Thrust; Engine; Aileron; Rudder
|The effectiveness of three exit vane cascade configurations for vectoring the thrust of a ducted fan - Mort, K. W.|
Effectiveness of three exit vane cascade configurations for thrust vectoring
Keywords: CASCADES; DUCTED FANS; THRUST VECTOR CONTROL; VANES; CASCADE; VANE
|NASA Connect - TOAT - Aerodynamic Forces - NASA LaRC Office of Education|
NASA Connect Segment that explains aerodynamic forces that affect aircraft performance and how these forces relate to each other.
Keywords: NASA Connect; Aerodynamic Force; Lift; Weight; Drag; Thrust
|Commodore C64 Manual: Jupiter Lander (1982)(Commodore)|
Commodore C64 Manual: Jupiter Lander (1982)(Commodore)
Keywords: thrust; landing; commodore; cartridge; jupiter; port; lander; joystick; korxj; sion
Keywords: arcadia; thrust; alien; row; cassette; attack; spaceship; plasma; score; left
|Effect on Gaseous Film Cooling of Coolant Injection Through Angled Slots and Normal Holes - Papell, S. Stephe|
A study was made to determine the effect of coolant injection angularity on gaseous film-cooling effectiveness. In the correlation of experimental data an effective injection angle was defined by a vector summation of the coolant and mainstream gas flows. The cosine of this angle was used as a parameter to empirically develop a corrective term to qualify a correlating equation presented in Technical Note D-130 that was limited to tangential injection of the coolant...
Keywords: RELATIVITY; ROCKETS; MOMENTUM; KINETIC ENERGY; ACCELERATION; MECHANICS (PHYSICS); ASTRONAUTS; THRUST
|Multiscale Analysis of Delamination of Carbon Fiber-Epoxy Laminates with Carbon Nanotubes - Riddick, Jaret C.|
A multi-scale analysis is presented to parametrically describe the Mode I delamination of a carbon fiber/epoxy laminate. In the midplane of the laminate, carbon nanotubes are included for the purposes of selectively enhancing the fracture toughness of the laminate. To analyze carbon fiber epoxy carbon nanotube laminate, the multi-scale methodology presented here links a series of parameterizations taken at various length scales ranging from the atomistic through the micromechanical to the struct...
Keywords: PULSEJET ENGINES; THRUST AUGMENTATION; EJECTORS; AUGMENTATION; CYLINDRICAL BODIES; THERMODYNAMIC CYCLES
|NASA SCI Files - Airplane Design - NASA LaRC Office of Education|
NASA Sci Files segment describing how airplane designer Burt Rutan takes projects from conception to reality, and the features that are the keys to flight.
Keywords: Burt Rutan; Boomerang; Proteus; Voyager; Imagination; Wing Span; Thrust
|User's manual for HESCOMP, the helicopter sizing and performance computer program - Davis, S. J.|
No Abstract Available
Keywords: MARS PROBES; THRUST AUGMENTATION; UNMANNED SPACECRAFT; DECELERATION; PAYLOADS; REENTRY